AeroLS Aerodynamic Lifting Surface Analysis
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AeroLS Tags

analysis surface control surface aerodynamic 3D modelling Surface Map Surface Explorer elliptic surface Surface test Glaciate surface surface implementation Surface Parametrizer Surface Reconstruction Unfold Surface aerodynamic analysis aerodynamic surface geometry analysis aerodynamic surface tension surface extrude simulate implicit surface surface analysis surface control analyze surface aerodynamic profile aerodynamic simulation Mean Aerodynamic Chord Aerodynamic Chord Calculator fibrous surface

AeroLS Description

The AeroLS application was designed to be an aerodynamic lifting surface analysis program. This means that it computes the effects of air flowing around thin (planform and camber only, no thickness) wings which are operating at a small angle of attack and sideslip in flow that is subsonic, steady, inviscid, and irrotational. AeroLS can be used to analyze any number of different lifting surfaces at a time, but can not analyze the effects of bodies such as fuselages in combination with wings. There are no limits (other than your computer's memory and solution run time) on the number of panels used to define your problem's geometry. Requirements: ￭ Java Runtime

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